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gptkbp:instanceOf
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gptkb:sports_championship
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gptkbp:aircraft
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gptkb:Mitsubishi_F-2
high maneuverability
low-wing
trainer aircraft
subsonic aircraft
jet aircraft
fly-by-wire system
multi-role capabilities
straight wing
modern aerodynamic design
twin-engine configuration
advanced flight control system
detailed specifications available.
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|
gptkbp:armament
|
none
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|
gptkbp:avionics
|
modern avionics system
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|
gptkbp:built
|
approximately 200
|
|
gptkbp:cockpit
|
glass cockpit
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|
gptkbp:communicationEquipment
|
secure communication system
|
|
gptkbp:constructionMaterial
|
all-metal construction
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|
gptkbp:crew
|
2
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gptkbp:crew_size
|
gptkb:Martin-Baker_ejection_seats
|
|
gptkbp:design
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:design_feature
|
high-mounted wings
|
|
gptkbp:engine
|
gptkb:NE-20_turbojet_engine
|
|
gptkbp:engineType
|
twin-engine
|
|
gptkbp:firstFlight
|
1988
|
|
gptkbp:fuel_capacity
|
2,500 liters
|
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gptkbp:height
|
4.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi T-4
|
|
gptkbp:introduced
|
1991
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|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
13.2 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:maximum_speed
|
1,000 km/h
|
|
gptkbp:maxTakeoffWeight
|
6,500 kg
|
|
gptkbp:missions
|
training and evaluation missions
|
|
gptkbp:navigationEquipment
|
inertial navigation system
|
|
gptkbp:operationalHistory
|
used_in_Japan_Air_Self-Defense_Force
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:primaryUser
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:productionYears
|
1988 to present
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:role
|
advanced trainer
lead-in fighter trainer
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:speed
|
110 km/h
|
|
gptkbp:succeededBy
|
50 degrees per second
|
|
gptkbp:successor
|
none
|
|
gptkbp:supportRole
|
basic and advanced training
|
|
gptkbp:surface
|
full-flying tail
|
|
gptkbp:team
|
Mitsubishi_design_team
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:variant
|
gptkb:T-4A
gptkb:T-4B
|
|
gptkbp:wingspan
|
12.3 m
|